Wind-Tunnel Investigation at High Subsonic Speeds of the Effects on Static Stability Characteristics of Various Modifications to a Swept-Wing Fighter-Type Airplane Model
1957
118 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft model , Fighter aircraft , Static stability , Swept wing , Wind tunnel stability test , Aircraft , Fighter , Fuselage , High speed , Model , Stability , Static , Subsonic , Sweep , Tail , Tunnel , Wind , Wing